This report discusses the development of a simulation model of an aircraft landing gear describing its typical non-linear behaviour. The development of the design tool -which correlates the actual design parameters with the performance of the gear- is a part of the research project that investigates the estimation of the nonlinear dynamical system, which an aircraft landing gear is. This project is a joint effort by the Eindhoven University of Technology and DAF Special Products.

    The non-linear parts of the simulation model are implemented in the general purpose multi body program DADS, which is based on time integration procedures.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    TIRE MODELS IN AIRCRAFT LANDING GEAR SIMULATION


    Beteiligte:

    Erschienen in:

    Vehicle System Dynamics ; 21 , sup1 ; 108-115


    Erscheinungsdatum :

    1992-01-01


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt



    Aircraft landing gear tire replacement frame

    BIAN HONGNING / LI YONGMING / KONG XINYI et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Aircraft landing gear tire anti-abrasion device

    WEI XIAOHUI / GAN YU / FANG XINGBO et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    TIRE SPACER INSTALLATION TOOL FOR AIRCRAFT LANDING GEAR

    Europäisches Patentamt | 2020

    Freier Zugriff

    TIRE SPACER INSTALLATION TOOL FOR AIRCRAFT LANDING GEAR

    YU YEONG HO | Europäisches Patentamt | 2020

    Freier Zugriff

    Landing Gear Design Impact on Aircraft Tire Life

    Zakrajsek, Andrew J. / Vogel, Ryan N. / Naboulsi, Sam et al. | AIAA | 2017